US8468676B2 - Method for securing a rotor to a motor drive shaft using cam fasteners - Google Patents
Method for securing a rotor to a motor drive shaft using cam fasteners Download PDFInfo
- Publication number
- US8468676B2 US8468676B2 US12/364,444 US36444409A US8468676B2 US 8468676 B2 US8468676 B2 US 8468676B2 US 36444409 A US36444409 A US 36444409A US 8468676 B2 US8468676 B2 US 8468676B2
- Authority
- US
- United States
- Prior art keywords
- bore
- motor shaft
- rotor
- fastener
- center point
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active, expires
Links
- 238000000034 method Methods 0.000 title claims description 18
- 230000001154 acute effect Effects 0.000 claims description 3
- 238000012423 maintenance Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 239000003550 marker Substances 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K1/00—Details of the magnetic circuit
- H02K1/06—Details of the magnetic circuit characterised by the shape, form or construction
- H02K1/22—Rotating parts of the magnetic circuit
- H02K1/28—Means for mounting or fastening rotating magnetic parts on to, or to, the rotor structures
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49002—Electrical device making
- Y10T29/49009—Dynamoelectric machine
- Y10T29/49012—Rotor
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49947—Assembling or joining by applying separate fastener
- Y10T29/49963—Threaded fastener
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T403/00—Joints and connections
- Y10T403/70—Interfitted members
- Y10T403/7018—Interfitted members including separably interposed key
- Y10T403/7021—Axially extending
- Y10T403/7024—Longitudinally stepped or tapered
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T403/00—Joints and connections
- Y10T403/70—Interfitted members
- Y10T403/7047—Radially interposed shim or bushing
- Y10T403/7051—Wedging or camming
Definitions
- the present invention relates to rotors, and in particular, to a magnetic encoded rotor incorporating a means for securing the rotor to a motor drive shaft, the means incorporating one or more cam-type fasteners.
- a first system is directed to a rotor having an external hub encircling and extending away from the central aperture.
- the external hub typically has a diameter less than the outer diameter of the rotor and extends from the face of the hub a relatively short distance.
- a plurality of set screws is inserted through holes in the hub to engage the motor shaft. Upon tightening, the set screws secure the rotor to the motor shaft.
- the external hub is typically positioned external to a stator housing, allowing the rotor to be repositioned after the stator housing is fixed in place.
- a known advantage of a modular encoder is having a thin axial profile, which is defeated by having an external hub. An external hub on a rotor adds thickness to the overall rotor, thereby negating the principal advantage of the modular encoder.
- the second method is similar to the first system wherein set screws are used to secure a rotor to the motor shaft.
- the set screws are positioned within the working thickness of the rotor such that they engage and tighten against the motor shaft through holes extending from the side edge of the rotor through the rotor's entire thickness.
- one of the tracks is typically a “marker” track which utilizes a small portion of the rotor's circumference so that the rest of the circumference on that side is available to locate the set screws. This allows the rotor to maintain its thin axial profile.
- the magnetic encoder rotor is located inside the stator housing, the side edge of the rotor is inaccessible after mounting the stator housing. A rotor cannot be repositioned, repaired, or replaced without removing the stator housing. Second, it is more difficult to reliably achieve maximum clamping force with set screw tightening tools.
- the third method is a rotor that is mostly hollow, having an internal hub with integral spokes connecting the internal hub with the outer edge of the rotor.
- two or three spokes connect the outer diameter to the inner diameter wherein the inner diameter matches the diameter of the motor shaft.
- One of the spokes has a slot in the center, which extends down through the inner diameter hub. This slot provides the extra space needed to fit the rotor on the motor shaft.
- a screw passes through the spoke with the slot such that upon tightening, the screw pinches the two halves of the slotted spoke together. This pinching action constricts the internal hub, tightening the rotor to the motor shaft.
- This system also has disadvantages. For example, it is more expensive to manufacture than using simple set screws.
- a fourth system and method for mounting a rotor to a motor shaft is a rotor having a tapered hub and is divided into two halves. This system then uses a split ring to tighten the hub around a motor shaft.
- a first, or female, half of the rotor has an inner diameter matching the motor shaft with one side having a tapered groove to the hub defining the inner diameter.
- a second, or male, half of the rotor is machined with a groove having a taper inverse of the first half.
- the split ring is contained within the tapered groove of this second half. Then, as the two halves are bolted together with screws, the split ring contained within the halves constricts, thereby tightening the hub of the rotor around the motor shaft.
- this system for mounting rotor on a motor shaft is more expensive than a set screw system. Also, in the best case, this system has a clamping force comparable to set screw systems. However, this system is subject to assembly errors. If the clamping screws are not tightened uniformly (or if the screw over the split in the split ring is tightened first), the clamping force is severely limited. There may be no immediate external indication of improper clamping, but such an improperly clamped rotor will slip during normal operation and cause system failures.
- cam fasteners such as cam screws
- the principal advantage to using cam screws is that they provide clamping forces equal to those found in traditional set screw methods while providing immediate access to the screws for maintenance purposes or for repositioning the rotor on the motor shaft without removing the stator housing.
- the cam screw rotor contains three pieces.
- the first is the rotor itself, which is a thin circular disk.
- the rotor has a central bore with a diameter approximately equal to the diameter of the motor shaft. Two holes are bored adjacent to the central bore such that each bore is adjacent to, and adjoining with, the central bore. Preferably each bore is aligned with a separate rotor axis.
- a conventional cam screw (having a head portion offset from a shaft portion) is screwed into each bore leaving the offset head portion clear of the central bore. After mounting the rotor on the motor shaft, the cam screws are rotated such that the eccentric heads contact the motor shaft with sufficient torque to prevent the rotor from slipping.
- this method is very simple. Manufacturing costs remain low in that the rotor itself has a very simple, straightforward design and conventional cam screws may be used. Second, the rotor can maintain a very narrow profile because the head portion of the cam screws may fit within a counter bore portion of the bores. Third, the cam screws for clamping the rotor to the rotor shaft are always accessible even after the stator housing is mounted. Fourth, for a given outer diameter, larger motor shaft sizes can be accommodated than those using the slotted spoke option. Fifth, this mounting system achieves clamping forces equal to or greater than that of set screw techniques, greater than those of the spoke style, and more consistent and less prone to failure than the split ring with tapered hub method.
- FIG. 1 is a planar front view of a rotor of the present invention
- FIG. 2 is a planar top view of the rotor
- FIG. 3 is a planar cross-sectional side view of the rotor
- FIG. 4 is a perspective view of the rotor assembly of the present invention.
- FIG. 5 is a perspective view of a cam fastener.
- FIGS. 1-3 show the preferred embodiment of a rotor 102 having a central bore 104 positioned about the intersection of a first, vertical, axis A and a second, horizontal, axis B wherein the first axis A is perpendicular to the second axis B.
- This central bore 104 has a diameter slightly larger than the diameter of the motor shaft.
- the rotor 102 has a first stepped bore 106 consisting of a tapped hole 110 through the thickness of the rotor 102 and a counterbored hole 108 .
- the tapped hole 110 and counterbored hole 108 are to accommodate the cam screw described below.
- the first stepped bore 106 is positioned adjacent to and adjoining with the central bore 104 aligned with the axis A such that the counterbored hole 108 intersects with the central bore 104 .
- first stepped bore 106 preferably aligns with the first axis A, but this is for convenience purpose only.
- the first stepped bore 106 may be positioned anywhere on the central bore 104 to achieve the same clamping forces needed to securely mount the rotor 102 to a motor shaft.
- the rotor 102 also has a second stepped bore 112 that is very similar to the first stepped bore 106 . That is, the second stepped bore 112 , preferably having a counterbored hole 114 and a tapped hole 116 , passes through the thickness of the rotor 102 and is adjacent to and adjoining with the central bore 104 along a portion of its circumference. However, the center point of the second stepped bore 112 preferably aligns with the second axis B, but this is for convenience purpose only.
- the second stepped bore 112 may be positioned anywhere on the central bore 104 to achieve the same clamping forces needed to securely mount the rotor 102 to a motor shaft. In one embodiment, an angle is made between said center point of said first bore, said center point of said central bore, and said center point of said second bore, wherein said angle is selected from the group consisting of acute angles, right angles, and obtuse angles.
- the rotor 102 of the present invention has a first face 118 , a second face 302 , and an outer edge 120 having grooves 202 .
- the rotor 102 is made of aluminum being about 3.7 inches in diameter and having a central bore 104 of about 0.6255 inches in diameter, 0.441 inches thick, and a first stepped bore 106 and a second stepped bore 112 with a counterbored hole 108 , 114 of about 0.375 inches in diameter and about 0.12 inches deep and a tapped hole 110 , 116 of about 0.25 inches in diameter.
- the center point of the first stepped bore 106 and the second stepped bore 112 is about 0.458 inches in length from the center point of the central bore 104 (or the intersection of axis A and axis B).
- the edge of the central bore 104 on both the first face 118 and the second face 302 may optionally have a small taper to facilitate the positioning of the rotor 102 on a motor shaft.
- such a taper may be 0.03 wide having a 45 degree angle.
- the present invention is described in terms of a first stepped bore 106 and a second stepped bore 112 for convenience purpose only. It would be readily apparent to one of ordinary skill in the relevant art to use a different number of stepped bores in the manner described herein, along different axes of the rotor 102 , to achieve the same clamping forces needed to securely mount the rotor 102 to a motor shaft.
- the rotor assembly 400 of the present invention of a rotor 102 mounted on a motor shaft 402 is shown in FIG. 4 , whereas the preferred cam fasteners used for such mounting means are cam screws 404 shown in detail in FIG. 5 .
- the preferred cam screw 404 used in the present invention is a conventional cam screw having a head portion 502 and a threaded shaft portion 504 wherein the head portion 502 is offset from the central longitudinal axis of the shaft portion 504 .
- a socket 506 in the head portion 502 is used for tightening and loosening the cam screw 404 .
- the preferred embodiment of cam fasteners are shown as cam screws 404 for convenience purpose only.
- the present invention can use any comparable cam fastener having an offset head.
- a cam screw 404 is inserted into each of the stepped bores 106 , 112 of the rotor 102 and then backed off until the head portion 502 of each cam screw 404 a,b has passed though the central bore 104 one time.
- the rotor 102 is positioned on the motor shaft 402 at a desired location.
- each cam screw 404 a,b is then rotated until the exterior edge 508 of each head portion 502 engages and is tightened against the motor shaft 402 .
- the exterior edge 508 of a cam screw 404 contacts the motor shaft 402 due to the offset design of the head portion 502 . Rotation of the cam screws 404 a, b is stopped once the desired clamping force is achieved.
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Abstract
Description
-
- This application is a divisional application of U.S. application Ser. No. 11/204,516, filed Aug. 16, 2005.
Claims (6)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/364,444 US8468676B2 (en) | 2005-08-16 | 2009-02-02 | Method for securing a rotor to a motor drive shaft using cam fasteners |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/204,516 US7485997B1 (en) | 2005-08-16 | 2005-08-16 | System and method for securing a rotor to a motor drive shaft using cam fasteners |
US12/364,444 US8468676B2 (en) | 2005-08-16 | 2009-02-02 | Method for securing a rotor to a motor drive shaft using cam fasteners |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/204,516 Division US7485997B1 (en) | 2005-08-16 | 2005-08-16 | System and method for securing a rotor to a motor drive shaft using cam fasteners |
Publications (2)
Publication Number | Publication Date |
---|---|
US20090133242A1 US20090133242A1 (en) | 2009-05-28 |
US8468676B2 true US8468676B2 (en) | 2013-06-25 |
Family
ID=40298072
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/204,516 Active 2026-07-28 US7485997B1 (en) | 2005-08-16 | 2005-08-16 | System and method for securing a rotor to a motor drive shaft using cam fasteners |
US12/364,444 Active 2026-06-23 US8468676B2 (en) | 2005-08-16 | 2009-02-02 | Method for securing a rotor to a motor drive shaft using cam fasteners |
US12/364,455 Active US7737601B2 (en) | 2005-08-16 | 2009-02-02 | System and method for securing a rotor to a motor drive shaft using cam fasteners |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/204,516 Active 2026-07-28 US7485997B1 (en) | 2005-08-16 | 2005-08-16 | System and method for securing a rotor to a motor drive shaft using cam fasteners |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US12/364,455 Active US7737601B2 (en) | 2005-08-16 | 2009-02-02 | System and method for securing a rotor to a motor drive shaft using cam fasteners |
Country Status (1)
Country | Link |
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US (3) | US7485997B1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20150082924A1 (en) * | 2013-09-19 | 2015-03-26 | Brent Morgan | Slew drive gearbox and clamp |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7244061B1 (en) * | 2004-01-21 | 2007-07-17 | Curtis David C | Marinating machine |
Citations (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US390583A (en) * | 1888-10-02 | Shaft and pulley coupling | ||
US1629113A (en) * | 1925-01-16 | 1927-05-17 | Maier William | Fastening device |
US1685899A (en) * | 1923-10-04 | 1928-10-02 | Kearney & Trecker Corp | Clamping device |
US1806694A (en) * | 1931-05-26 | Locking mechanism | ||
US2430613A (en) * | 1945-03-15 | 1947-11-11 | Robert W Hodge | Work holding means |
US3501183A (en) * | 1965-06-29 | 1970-03-17 | Andrew Stratienko | Linear self-interlocking wedge device |
US4089611A (en) * | 1975-12-17 | 1978-05-16 | Vereinigte Osterreichische Eisen- Und Stahlwerke Alpine Montan Aktiengesellschaft | Releasable hub-shaft connection mechanism |
US4157819A (en) * | 1977-01-27 | 1979-06-12 | Meyer Richard W | Adjustable work piece clamping system |
US4477064A (en) * | 1982-06-09 | 1984-10-16 | Digiulio Mario | Device for holding work in machine tool operations |
US4789287A (en) * | 1985-07-18 | 1988-12-06 | Nixdorf Computer Ag | Through bolt connection for unilaterally accessible locations |
US4934042A (en) | 1987-10-16 | 1990-06-19 | Bush Timothy J | Lamination to rotor shaft retention method utilizing spring pins |
US5310299A (en) * | 1992-09-01 | 1994-05-10 | Kurt Manufacturing Company, Inc. | Sliding clamp |
US5641257A (en) * | 1992-09-01 | 1997-06-24 | Kurt Manufacturing Company, Inc. | Sliding clamp |
US5657971A (en) * | 1995-08-11 | 1997-08-19 | Williams; Willis Ray | Abutment plate workpiece clamping apparatus |
US5657974A (en) * | 1994-05-16 | 1997-08-19 | Williams; Willis Ray | Workpiece clamping apparatus for a collapsible work bench |
US5671915A (en) * | 1995-08-11 | 1997-09-30 | Williams; Willis Ray | Locking cam workpiece clamping apparatus |
US5718421A (en) | 1996-11-06 | 1998-02-17 | Cimino; Michael A. | Orbital hold-down clamp |
US5833225A (en) * | 1995-11-13 | 1998-11-10 | Weber; Gene | Gripping device |
US5902066A (en) * | 1997-07-10 | 1999-05-11 | Lake Shore Cryotronics, Inc. | Taper shaft lock |
US6037696A (en) | 1993-12-29 | 2000-03-14 | Samot Engineering (1992) Ltd. | Permanent magnet axial air gap electric machine |
JP2004286155A (en) | 2003-03-24 | 2004-10-14 | Tsubaki Emerson Co | Friction-type fastener for fastening shaft to rotor |
JP2006194083A (en) | 2003-09-16 | 2006-07-27 | Boc Edwards Kk | Structure for fixing rotor shaft and rotating body and turbomolecular pump having the structure |
-
2005
- 2005-08-16 US US11/204,516 patent/US7485997B1/en active Active
-
2009
- 2009-02-02 US US12/364,444 patent/US8468676B2/en active Active
- 2009-02-02 US US12/364,455 patent/US7737601B2/en active Active
Patent Citations (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US390583A (en) * | 1888-10-02 | Shaft and pulley coupling | ||
US1806694A (en) * | 1931-05-26 | Locking mechanism | ||
US1685899A (en) * | 1923-10-04 | 1928-10-02 | Kearney & Trecker Corp | Clamping device |
US1629113A (en) * | 1925-01-16 | 1927-05-17 | Maier William | Fastening device |
US2430613A (en) * | 1945-03-15 | 1947-11-11 | Robert W Hodge | Work holding means |
US3501183A (en) * | 1965-06-29 | 1970-03-17 | Andrew Stratienko | Linear self-interlocking wedge device |
US4089611A (en) * | 1975-12-17 | 1978-05-16 | Vereinigte Osterreichische Eisen- Und Stahlwerke Alpine Montan Aktiengesellschaft | Releasable hub-shaft connection mechanism |
US4157819A (en) * | 1977-01-27 | 1979-06-12 | Meyer Richard W | Adjustable work piece clamping system |
US4477064A (en) * | 1982-06-09 | 1984-10-16 | Digiulio Mario | Device for holding work in machine tool operations |
US4789287A (en) * | 1985-07-18 | 1988-12-06 | Nixdorf Computer Ag | Through bolt connection for unilaterally accessible locations |
US4934042A (en) | 1987-10-16 | 1990-06-19 | Bush Timothy J | Lamination to rotor shaft retention method utilizing spring pins |
US5310299A (en) * | 1992-09-01 | 1994-05-10 | Kurt Manufacturing Company, Inc. | Sliding clamp |
US5641257A (en) * | 1992-09-01 | 1997-06-24 | Kurt Manufacturing Company, Inc. | Sliding clamp |
US6037696A (en) | 1993-12-29 | 2000-03-14 | Samot Engineering (1992) Ltd. | Permanent magnet axial air gap electric machine |
US5657974A (en) * | 1994-05-16 | 1997-08-19 | Williams; Willis Ray | Workpiece clamping apparatus for a collapsible work bench |
US5657971A (en) * | 1995-08-11 | 1997-08-19 | Williams; Willis Ray | Abutment plate workpiece clamping apparatus |
US5671915A (en) * | 1995-08-11 | 1997-09-30 | Williams; Willis Ray | Locking cam workpiece clamping apparatus |
US5833225A (en) * | 1995-11-13 | 1998-11-10 | Weber; Gene | Gripping device |
US5718421A (en) | 1996-11-06 | 1998-02-17 | Cimino; Michael A. | Orbital hold-down clamp |
US5902066A (en) * | 1997-07-10 | 1999-05-11 | Lake Shore Cryotronics, Inc. | Taper shaft lock |
JP2004286155A (en) | 2003-03-24 | 2004-10-14 | Tsubaki Emerson Co | Friction-type fastener for fastening shaft to rotor |
JP2006194083A (en) | 2003-09-16 | 2006-07-27 | Boc Edwards Kk | Structure for fixing rotor shaft and rotating body and turbomolecular pump having the structure |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20150082924A1 (en) * | 2013-09-19 | 2015-03-26 | Brent Morgan | Slew drive gearbox and clamp |
US9353781B2 (en) * | 2013-09-19 | 2016-05-31 | Brent Morgan | Slew drive gearbox and clamp |
Also Published As
Publication number | Publication date |
---|---|
US7737601B2 (en) | 2010-06-15 |
US7485997B1 (en) | 2009-02-03 |
US20090134741A1 (en) | 2009-05-28 |
US20090133242A1 (en) | 2009-05-28 |
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